Check valve

- Allied-Signal Inc.

A check valve for use in the evacuation of air from a system having primary and secondary disc retained in a chamber of the housing and responsive to first and second forces developed by the creation of a fluid pressure differential between the fluid pressure of air in a first member and a source of vacuum to control the evacuation of air from the member by the source of vacuum. The primary disc is located on a stem that extends from the secondary disc to cover a plurality of openings which connect the inlet port to the chamber. A spring holds the secondary disc against the housing. The first force which develops as a result of a pressure differential between the fluid pressure of air and vacuum moves the primary disc to allow air to be evacuated through the openings in the secondary disc. Should the fluid pressure in the air located in the first member exceed a predetermined value, the second force develops which acts on the secondary disc to allow a larger volume of air to be evacuated in a shorter time. A tang on the secondary disc engages the housing to prevent the development of vibrations therein when air is evacuated as a result of movement by the secondary disc. When the fluid pressure of the air is reduced to a predetermined fluid pressure, a spring moves the secondary disc into engagement with the housing and the evacuation of air is again through the openings in the secondary disc as controlled by the first disc.

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Description

These object and others should be apparent from reading this specification while viewing the drawings wherein:

FIG. 1 is a sectional view of a check valve made according to the principles of this invention when the fluid pressure of fluid in a system is substantially the same at the inlet port and the outlet port;

FIG. 2 is a sectional view of the check valve of FIG. 1 wherein fluid flow from the inlet port to the outlet port is controlled by the primary disc member in response to a first pressure differential level in the fluid between the inlet port and the outlet port; and

FIG. 3 is a sectional view of the check valve of FIG. 1 wherein fluid flow from the inlet port to the outlet port is controlled by the secondary disc member in response to a second pressure differential level in the fluid between the inlet port and the outlet port.

DETAILED DESCRIPTION

The check valve 10 shown in FIG. 1 has a housing 12 with a bore 14 therein. Housing 12 has an inlet port 16 which is adapted to be connected to a power assist booster and an outlet port 18 which is adapted to be connected to a source of vacuum, typically the inlet manifold of an internal combustion engine. Housing 12 has a groove 20 located in bore 14 for retaining end cap 22 and aligning guide 24 therein with guide 26 located in inlet port 16. With end cap located in groove 20, a chamber 28 is formed in housing 12 between the inlet port 16 and outlet port 18. Housing 12 has a groove 30 which forms a step or extension of bore 14 surrounds inlet port 16 and directs the flow of air into check valve 10. The evacuation of air from the power assist booster through the check valve 10 to the source of vacuum is controlled by primary and secondary disc members 32 and 34, respectively, located in chamber 28. The primary disc member 32 which is carried by the secondary disc member 34 controls the evacuation of air when the fluid pressure in the power assist booster approaches the fluid pressure of the source of vacuum while the secondary disc member 34 controls the evacuation of air when the fluid pressure differential exceeds a predetermined value.

The secondary disc member 34 has a body 36 with a first stem 38 that extends from substantially the center thereof into guide 24 and a second stem 40 that extends into guide 26, a plurality of openings 42, 42' that surround the first and second stems 38 and 40, an annular seat 41 which surrounds the plurality of openings 42, 42' and a peripheral surface 44 thereon. A resilient flange member 46 which surrounds peripheral surface 44 has an annular rib 48 that is designed to engage housing 12 and seal groove 30 from chamber 28. The resilient flange member 46 has at least one, and depending upon the expected air flow through chamber 28, tang 50 which engages the side wall of bore 14 the purpose of which will be explained later with respect to the functional operation of check valve 10.

The primary disc member 32 is retained on the first stem 38 by a shoulder 37. The primary disc member 32 which is initially substantially parallel to the secondary disc member 34 is flexible and when placed on stem 38 assumes a concave shape on engagement with annular seat 41 as shown in FIG. 1 to cover the plurality of openings 42, 42' in the secondary disc member 34.

A spring or resilient means 52 located between end cap 22 and body 36 of the secondary disc member 34 urges rib 48 on flange member 44 into engagement with the housing surrounding groove 30 to normally seal chamber 28 from the inlet port 16.

MODE OF OPERATION

When an internal combustion engine is operating, vacuum is produced and communicated to outlet port 18 of check valve 10 by an appropriate conduit. Air in a power assist booster having a fluid pressure greater than the level of vacuum communicated to inlet port 16 develops an operational pressure differential between the inlet port 16 and outlet port 18. In the absence of a brake application, this operational pressure differential would be low and may not be sufficient to move either the primary or secondary disc members 32 and 34 away from their respective seats to alleviated the operational pressure differential. However, assume that a brake application has occurred and some air has been communicated into the brake system by way of the power assist booster sufficient to develop a pressure differential between the inlet port 16 and outlet port 18. This operational pressure differential acts on the primary disc member 32 and secondary disc member 34 to produce an operational force. When the operational force is less than the spring force of spring 52, the operational pressure differential creates a first force which acts on and moves the primary disc member 32 away from seat 41, as illustrated in FIG. 2, to allow air to be evacuated from the power assist booster by flowing through the plurality of openings 42, 42' to reduce the fluid pressure of the air in the power assist booster to substantially the fluid pressure of the vacuum presented to outlet port 18.

When the operational pressure differential is greater than the spring force of spring 52, a second operational differential pressure is created to develop a second force which acts on the primary and secondary disc members 32 and 34 as illustrated in FIG. 3 to overcome the spring force and move annular rib 48 on flange 44 away from housing 12 to allow air to be directly evacuated from the power assist booster by flowing from groove 30 to the outlet port 18 to rapidly lower the fluid pressure of air. As the secondary disc member 34 moves in chamber 28 the engagement of stems 38 and 40 with guides 24 and 26 respectively keeps the flange member 44 aligned over its seat in housing 12. As the air is rapidly evacuated from the power assist booster, turbulence can occur in the flow because of engagement with ribs and the unstable conditions caused by the varying force relationship between the spring force and second pressure differential force and as a result it is possible to create harmonic vibrations in the second disc member 34. When the second disc member 34 moves within chamber 28, tang 50 engages bore 14 to attenuate the development of vibrations to aid in maintaining the second disc member 34 in a stable condition. While only one tang 50 is shown, in some brake systems where a considerable volume of air is required to be evacuated from the power assist booster it may be necessary to provide additional tangs to maintain such stability. When the fluid pressure of the air in the power assist booster has been sufficiently reduced, the spring force of spring 52 again acts on the secondary disc member 34 to move annular rib 48 on flange into a seating position on housing 12 to terminate the flow air from the inlet port 16 by way of the groove 30 and reinstitute the evacuation of air through plurality of openings 42, 42' under the control of the primary disc member 32. Thereafter evacuation occurs through the primary disc member as illustrated in FIG. 2 until the fluid pressure in the power assist booster is substantially equal to the source of vacuum and the internal resiliency of the primary disc member 32 returns or repositions the primary disc member 32 on annular seat 41 as shown in FIG. 1 to seal the inlet port 16 from the outlet port 18.

Claims

1. A check valve for use in the evacuation of air from a system, comprising:

a housing having a chamber with a groove connected to an inlet port, said inlet port being connected to a first member in said system, said chamber having an outlet port connected to a source of vacuum;
primary and secondary disc members located in said chamber for controlling the evacuation of air from said first member by said source of vacuum;
said secondary disc member having a first stem that extends from substantially the center thereof, a plurality of openings that surround said first stem and a peripheral surface thereon, said first stem having a shoulder thereon, said first stem being retained in a first guide for locating said peripheral surface over said groove in said housing;
said primary disc member being flexibly retained on said first stem of said secondary disc member by said shoulder, said primary disc member being substantially parallel to said secondary disc member and extending to cover said plurality of openings therein; and
resilient means located in said chamber for urging said peripheral surface on said secondary disc member into engagement with said housing, said source of vacuum and any air in said first member developing an operational pressure differential across said primary and secondary disc members, when said operational pressure differential is less then that of the spring force of said resilient means a first pressure differential creates a first force which moves said primary disc member away from said plurality of openings to allow said vacuum to evacuate air from the first member and to reduce the fluid pressure of the air in said first member to substantially the fluid pressure of said source of vacuum and when said operational pressure differential is greater than said spring force a second operational pressure differential creates a second force which overcomes said resilient means to move said secondary disc member and peripheral surface thereon away from said housing to allow air to flow from the inlet port through the chamber to the outlet port to lower the fluid pressure of air in the first member to a fluid pressure where the force of the resilient means against moves said peripheral surface back into engagement with said housing to terminate the flow of air from the inlet port by way of the groove and reinstitute air flow from said first member to the outlet port through said plurality of openings until the fluid pressure in said first member is substantially equal to said source of vacuum.

2. The check valve for use in the evacuation of air from a system as recited in claim 1 wherein said secondary disc member includes:

a flange member which surrounds said peripheral surface, said flange member having an annular rib that engages said housing to seal said groove from said chamber once the fluid pressure for developing said first fluid pressure differential is obtained.

3. The check valve for use in evacuation of air from a system as recited in claim 2 wherein said flange member includes:

a tang that extends to and engages said housing to attenuate harmonic vibration in said secondary disc member when air flows between said annular rib and the housing to the outlet port.

4. The check valve for use in the evacuation of air from a system as recited in claim 3 wherein said secondary disc member further includes:

a second stem extending from said secondary disc member and engaging a second guide in said housing to maintain said secondary disc in alignment over said groove.

5. The check valve for use in the evacuation of air from a system as recited in claim 4 wherein said tang provides a lateral extension which maintains said secondary disc member in axial alignment within the chamber to further prevent harmonic vibrations in said secondary member.

6. The check valve for use in evacuation of air from a system as recited in claim 2 wherein said flange member includes:

a plurality of tangs that extends to and engages said housing to maintain said secondary disc member in axial alignment within said chamber and attenuate harmonic vibration in said secondary disc member when air flows between said annular rib and the housing to the outlet port.
Referenced Cited
U.S. Patent Documents
2296492 September 1942 Begley
2947314 August 1960 Bloom
4886085 December 12, 1989 Miller
Patent History
Patent number: 5117860
Type: Grant
Filed: Oct 22, 1991
Date of Patent: Jun 2, 1992
Assignee: Allied-Signal Inc. (Morristown, NJ)
Inventor: Charles B. Horner, Jr. (South Bend, IN)
Primary Examiner: Robert G. Nilson
Attorneys: Leo H. McCormick, Jr., Ken C. Decker
Application Number: 7/781,545
Classifications
Current U.S. Class: 137/5121; 137/5122; 137/5123; Vacuum Relief Type (137/526)
International Classification: F16K 1502;